@InProceedings{Macau:2019:FoDyEx,
author = "Macau, Elbert Einstein Nehrer",
affiliation = "{Instituto Nacional de Pesquisas Espaciais (INPE)}",
title = "Building inclinated and excentric high earth orbits through small
perturbations: a four-body dynamics exploration",
year = "2019",
organization = "International Astronautical Congress, 70.; IAF Astrodynamics
Symposium",
abstract = "In specific applications, such as communication missions, require
orbits with large journey time between the apogee and perigee,
thus remaining for long periods at a specific point in space.
Normally in these cases, the final inclination, eccentricity and
semimajor axis values aimed demand too much fuel consumption when
conducted by the conventional transfers methods. In this work, an
alternative strategy transfer is proposed. It consists of
exploring and take advantage of the natural dynamics associated to
the unstable orbits and sensitive dependence present in the four
body problem. In this perspective, a low cost transfer starting
from a low to a high and inclinated Earth orbit is built through a
combination of a lunar gravity assisted maneuver and the
application of judicious and small impulses to specific points of
the trajectory. The method was validated in case studies carried
out for a scenario composed of Sun, Earth, Moon and vehicle. The
results obtained show that it is possible to obtain the desired
stable orbits with a low total impulse magnitude, even in cases
where conventional transfer methods are not feasible.",
conference-location = "Washington, DC",
conference-year = "21-25 Oct.",
language = "en",
targetfile = "macau_building.pdf",
urlaccessdate = "11 abr. 2021"
}